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- Title
Starting of an axisymmetric convergent-divergent nozzle in a hypersonic flow.
- Authors
Zubin, M.; Tunik, Yu.
- Abstract
The starting of an axisymmetric convergent-divergent nozzle, with the result that supersonic flow is formed within almost the entire channel, is modeled, as applied to the hypersonic aerodynamic setup of the Institute of Mechanics of Moscow State University. A successful starting is realized when the nozzle is thrown in a uniform supersonic air flow at a fairly high Mach number. The steady flow structure is studied. It is numerically shown that in the convergent section of the channel there arises an oblique shock wave whose interaction with the nozzle axis leads to the formation of a reflected shock and a curvilinear Mach disk with a region of unsteady subsonic flow in the vicinity of the throat. The mathematical model is based on the two-dimensional Euler equations for axisymmetric gas flows.
- Subjects
NOZZLES; FLUID dynamics; AXIAL flow; HYPERSONIC flow; AERODYNAMICS; AIR flow; SHOCK waves; EULER equations; MOSCOW State University
- Publication
Fluid Dynamics, 2014, Vol 49, Issue 4, p557
- ISSN
0015-4628
- Publication type
Article
- DOI
10.1134/S0015462814040164